科技报告详细信息
| Optimization of Second Fault Detection Thresholds to Maximize Mission Probability of Success | |
| Anzalone, Evan | |
| 关键词: SPACE LAUNCH SYSTEM (SLS); DESIGN OPTIMIZATION; FAULT DETECTION; PROBABILITY THEORY; COMPLEX SYSTEMS; NAVIGATION; SPECIFICATIONS; TOLERANCES (MECHANICS); PAYLOADS; ACCURACY; COMPUTERIZED SIMULATION; MONTE CARLO METHOD; | |
| RP-ID : M18-6519 | |
| 学科分类：航空航天科学 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| 20180002047.pdf | 394KB |  download |
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